Control of Flow Separation over a Flapped Airfoil Using Low-Aspect-Ratio Circular Pins
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, New York 12180
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056883
Reference17 articles.
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2. HuangL. S.MaestrelloL.BryantT. D. “Separation Control over an Airfoil at High Angles of Attack by Sound Emanating from the Surface,” AIAA Paper 1987-1261, 1987.
3. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation
4. ReneW.HolgerN.RaghuS.WygnanskiI. “Parametric Study of Sweeping Jet Actuators for Separation Control,” AIAA Paper 2010-4247, 2010.
5. CorkeT. “Overview of Plasma Flow Control: Concepts, Optimization, and Applications,” AIAA Paper 2005-0563, 2005.
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